FR2881008B1 - SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY - Google Patents
SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITYInfo
- Publication number
- FR2881008B1 FR2881008B1 FR0500592A FR0500592A FR2881008B1 FR 2881008 B1 FR2881008 B1 FR 2881008B1 FR 0500592 A FR0500592 A FR 0500592A FR 0500592 A FR0500592 A FR 0500592A FR 2881008 B1 FR2881008 B1 FR 2881008B1
- Authority
- FR
- France
- Prior art keywords
- satellite
- calculates
- receiver
- pseudo
- instantaneous
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/43—Determining position using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
- G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Fire Alarms (AREA)
Abstract
The invention relates to a receiver of signals of a satellite-based radionavigation system intended to calculate the position of a carrier very precisely. The receiver comprises several digital signal processing channels each associated with a satellite and each providing a first digital datum representing a pseudo-distance between the receiver and the satellite in the form of an instantaneous temporal position of a pseudo-random code and a second digital datum representing this pseudo-distance in the form of an instantaneous phase of the carrier of the signal transmitted by the satellite. According to the invention, the receiver comprises an extended Kalman filter. The Kalman filter for calculates an instantaneous position of the receiver, means for calculates propagation of a state vector, calculates registration of the state vector on the basis of observations relating to each satellite and of a matrix of observations. The Kalman filter calculates observation and calculates an estimated instantaneous pseudo-distance for each satellite.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0500592A FR2881008B1 (en) | 2005-01-20 | 2005-01-20 | SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY |
CA2589463A CA2589463C (en) | 2005-01-20 | 2006-01-03 | Improved integrity and continuity satellite positioning receiver |
US11/814,409 US7504996B2 (en) | 2005-01-20 | 2006-01-03 | Satellite-based positioning receiver with improved integrity and continuity |
DE602006002367T DE602006002367D1 (en) | 2005-01-20 | 2006-01-03 | ITY AND CONTINUITY |
AT06700317T ATE405852T1 (en) | 2005-01-20 | 2006-01-03 | SATELLITE RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY |
EP06700317.8A EP1839070B2 (en) | 2005-01-20 | 2006-01-03 | Improved integrity and continuity satellite positioning receiver |
PCT/EP2006/050014 WO2006077174A1 (en) | 2005-01-20 | 2006-01-03 | Improved integrity and continuity satellite positioning receiver |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0500592A FR2881008B1 (en) | 2005-01-20 | 2005-01-20 | SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2881008A1 FR2881008A1 (en) | 2006-07-21 |
FR2881008B1 true FR2881008B1 (en) | 2007-04-20 |
Family
ID=34954333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0500592A Expired - Fee Related FR2881008B1 (en) | 2005-01-20 | 2005-01-20 | SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY |
Country Status (7)
Country | Link |
---|---|
US (1) | US7504996B2 (en) |
EP (1) | EP1839070B2 (en) |
AT (1) | ATE405852T1 (en) |
CA (1) | CA2589463C (en) |
DE (1) | DE602006002367D1 (en) |
FR (1) | FR2881008B1 (en) |
WO (1) | WO2006077174A1 (en) |
Families Citing this family (81)
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US8203486B1 (en) | 1999-03-05 | 2012-06-19 | Omnipol A.S. | Transmitter independent techniques to extend the performance of passive coherent location |
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US7570214B2 (en) | 1999-03-05 | 2009-08-04 | Era Systems, Inc. | Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surviellance |
US7908077B2 (en) | 2003-06-10 | 2011-03-15 | Itt Manufacturing Enterprises, Inc. | Land use compatibility planning software |
US7777675B2 (en) * | 1999-03-05 | 2010-08-17 | Era Systems Corporation | Deployable passive broadband aircraft tracking |
US7782256B2 (en) | 1999-03-05 | 2010-08-24 | Era Systems Corporation | Enhanced passive coherent location techniques to track and identify UAVs, UCAVs, MAVs, and other objects |
US7948769B2 (en) | 2007-09-27 | 2011-05-24 | Hemisphere Gps Llc | Tightly-coupled PCB GNSS circuit and manufacturing method |
US7885745B2 (en) | 2002-12-11 | 2011-02-08 | Hemisphere Gps Llc | GNSS control system and method |
US8265826B2 (en) | 2003-03-20 | 2012-09-11 | Hemisphere GPS, LLC | Combined GNSS gyroscope control system and method |
US8190337B2 (en) | 2003-03-20 | 2012-05-29 | Hemisphere GPS, LLC | Satellite based vehicle guidance control in straight and contour modes |
US8138970B2 (en) | 2003-03-20 | 2012-03-20 | Hemisphere Gps Llc | GNSS-based tracking of fixed or slow-moving structures |
US8634993B2 (en) | 2003-03-20 | 2014-01-21 | Agjunction Llc | GNSS based control for dispensing material from vehicle |
US8271194B2 (en) | 2004-03-19 | 2012-09-18 | Hemisphere Gps Llc | Method and system using GNSS phase measurements for relative positioning |
US9002565B2 (en) | 2003-03-20 | 2015-04-07 | Agjunction Llc | GNSS and optical guidance and machine control |
US8594879B2 (en) | 2003-03-20 | 2013-11-26 | Agjunction Llc | GNSS guidance and machine control |
US8686900B2 (en) * | 2003-03-20 | 2014-04-01 | Hemisphere GNSS, Inc. | Multi-antenna GNSS positioning method and system |
US8140223B2 (en) | 2003-03-20 | 2012-03-20 | Hemisphere Gps Llc | Multiple-antenna GNSS control system and method |
FR2863814B1 (en) * | 2003-12-16 | 2006-04-28 | Cit Alcatel | METHOD OF UPDATING THE BIT OF CLOCK EXISTING BETWEEN A BTS STATION OF A GSM NETWORK AND THE SATELLITES OF A GPS SYSTEM |
US8583315B2 (en) | 2004-03-19 | 2013-11-12 | Agjunction Llc | Multi-antenna GNSS control system and method |
US8107540B2 (en) * | 2005-07-11 | 2012-01-31 | Cheetah Technologies, L.P. | Image complexity computation in packet based video broadcast systems |
US7739032B2 (en) * | 2006-03-21 | 2010-06-15 | Broadcom Corporation | Method and apparatus for generating and using a regional-terrain model |
US7965227B2 (en) | 2006-05-08 | 2011-06-21 | Era Systems, Inc. | Aircraft tracking using low cost tagging as a discriminator |
US7835832B2 (en) | 2007-01-05 | 2010-11-16 | Hemisphere Gps Llc | Vehicle control system |
US8311696B2 (en) | 2009-07-17 | 2012-11-13 | Hemisphere Gps Llc | Optical tracking vehicle control system and method |
USRE48527E1 (en) | 2007-01-05 | 2021-04-20 | Agjunction Llc | Optical tracking vehicle control system and method |
US8000381B2 (en) | 2007-02-27 | 2011-08-16 | Hemisphere Gps Llc | Unbiased code phase discriminator |
FR2913773B1 (en) * | 2007-03-16 | 2014-08-01 | Thales Sa | DEVICE FOR RECEIVING SATELLITE SIGNALS COMPRISING A PHASE LOOP WITH DELAY COMPENSATION |
FR2916551B1 (en) * | 2007-05-25 | 2009-07-10 | Thales Sa | SIGNAL PROCESSING DEVICE OF SYSTEMS IN DIFFERENTIAL CONFIGURATION. |
DE102008046896A1 (en) * | 2007-09-13 | 2009-04-16 | Continental Teves Ag & Co. Ohg | Security-critical map update via a data channel of a satellite navigation system |
US7808428B2 (en) | 2007-10-08 | 2010-10-05 | Hemisphere Gps Llc | GNSS receiver and external storage device system and GNSS data processing method |
US9002566B2 (en) | 2008-02-10 | 2015-04-07 | AgJunction, LLC | Visual, GNSS and gyro autosteering control |
WO2009126587A1 (en) | 2008-04-08 | 2009-10-15 | Hemisphere Gps Llc | Gnss-based mobile communication system and method |
WO2010059299A2 (en) * | 2008-10-06 | 2010-05-27 | Viasat, Inc. | Synchronization for mesh satellite communications |
US7961141B2 (en) * | 2008-12-09 | 2011-06-14 | Navcom Technology, Inc. | Methods and systems to increase accuracy in the navigation of single frequency receivers |
US8217833B2 (en) | 2008-12-11 | 2012-07-10 | Hemisphere Gps Llc | GNSS superband ASIC with simultaneous multi-frequency down conversion |
US8386129B2 (en) | 2009-01-17 | 2013-02-26 | Hemipshere GPS, LLC | Raster-based contour swathing for guidance and variable-rate chemical application |
US8085196B2 (en) | 2009-03-11 | 2011-12-27 | Hemisphere Gps Llc | Removing biases in dual frequency GNSS receivers using SBAS |
US8401704B2 (en) | 2009-07-22 | 2013-03-19 | Hemisphere GPS, LLC | GNSS control system and method for irrigation and related applications |
US8174437B2 (en) | 2009-07-29 | 2012-05-08 | Hemisphere Gps Llc | System and method for augmenting DGNSS with internally-generated differential correction |
US8334804B2 (en) | 2009-09-04 | 2012-12-18 | Hemisphere Gps Llc | Multi-frequency GNSS receiver baseband DSP |
US8649930B2 (en) | 2009-09-17 | 2014-02-11 | Agjunction Llc | GNSS integrated multi-sensor control system and method |
US8548649B2 (en) | 2009-10-19 | 2013-10-01 | Agjunction Llc | GNSS optimized aircraft control system and method |
FR2954521B1 (en) * | 2009-12-18 | 2012-04-20 | Thales Sa | SATELLITE POSITIONING RECEIVER |
US20110188618A1 (en) * | 2010-02-02 | 2011-08-04 | Feller Walter J | Rf/digital signal-separating gnss receiver and manufacturing method |
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US9829582B2 (en) * | 2011-09-19 | 2017-11-28 | Raytheon Company | Method and apparatus for differential global positioning system (DGPS)-based real time attitude determination (RTAD) |
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US10215862B2 (en) * | 2014-04-07 | 2019-02-26 | Honeywell International Inc. | Systems and methods for a code carrier divergence high-pass filter monitor |
US9933528B2 (en) | 2014-10-27 | 2018-04-03 | Swift Navigation, Inc. | Systems and methods for real time kinematic satellite positioning |
US10114126B2 (en) | 2015-04-30 | 2018-10-30 | Raytheon Company | Sensor installation monitoring |
US10551196B2 (en) | 2015-04-30 | 2020-02-04 | Raytheon Company | Sensor installation monitoring |
FR3049354B1 (en) * | 2016-03-25 | 2018-03-16 | Thales | SATELLITE GEOPOSITIONING METHOD AND ASSOCIATED TERMINAL |
US10247829B2 (en) | 2016-08-10 | 2019-04-02 | Raytheon Company | Systems and methods for real time carrier phase monitoring |
US10473790B2 (en) | 2017-11-17 | 2019-11-12 | Swift Navigation, Inc. | Systems and methods for distributed dense network processing of satellite positioning data |
US10578747B2 (en) | 2017-12-14 | 2020-03-03 | Swift Navigation, Inc. | Systems and methods for reduced-outlier satellite positioning |
EP3502747B1 (en) * | 2017-12-22 | 2020-06-10 | Trimble Inc. | Advanced navigation satellite system positioning method and system using seeding information |
KR20210152549A (en) | 2019-05-01 | 2021-12-15 | 스위프트 내비게이션, 인크. | Systems and methods for high-integrity satellite positioning |
CN114502987A (en) | 2019-08-01 | 2022-05-13 | 斯威夫特导航股份有限公司 | System and method for GNSS correction generation for gaussian process augmentation |
US11016199B1 (en) | 2019-12-11 | 2021-05-25 | Swift Navigation, Inc. | System and method for validating GNSS ambiguities |
WO2021202004A2 (en) | 2020-02-14 | 2021-10-07 | Swift Navigation, Inc. | System and method for reconverging gnss position estimates |
US11714200B2 (en) | 2020-03-18 | 2023-08-01 | Honeywell International Inc. | Single-difference based pre-filter of measurements for use in solution separation framework |
US11460585B2 (en) | 2020-03-18 | 2022-10-04 | Honeywell International Inc. | Implementing single differences within a solution separation framework |
WO2021252638A1 (en) | 2020-06-09 | 2021-12-16 | Swift Navigation, Inc. | System and method for satellite positioning |
CN112051598B (en) * | 2020-06-24 | 2023-09-29 | 中铁第四勘察设计院集团有限公司 | Dual-correction-based vehicle-mounted GNSS/INS integrated navigation method |
CN116261676A (en) | 2020-07-13 | 2023-06-13 | 斯威夫特导航股份有限公司 | System and method for determining GNSS positioning corrections |
WO2022046317A2 (en) | 2020-07-17 | 2022-03-03 | Swift Navigation, Inc. | System and method for providing gnss corrections |
CN111948686B (en) * | 2020-08-05 | 2024-04-26 | 航天恒星科技有限公司 | Time synchronization method and device |
FR3113943B1 (en) * | 2020-09-09 | 2022-08-19 | Commissariat Energie Atomique | A method of determining the position and orientation of a vehicle. |
DE102020213315A1 (en) * | 2020-10-22 | 2022-04-28 | Robert Bosch Gesellschaft mit beschränkter Haftung | Method for GNSS-based localization of a vehicle with a GNSS localization device, taking into account integrity information that is provided for GNSS correction data |
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WO2023167916A1 (en) | 2022-03-01 | 2023-09-07 | Swift Navigation, Inc. | System and method for detecting outliers in gnss observations |
WO2024050094A1 (en) | 2022-09-01 | 2024-03-07 | Swift Navigation, Inc. | System and method for determining gnss corrections |
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FR3141580A1 (en) * | 2022-10-27 | 2024-05-03 | Thales | Accurate time broadcasting method integrates |
Family Cites Families (5)
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FR2769442B1 (en) * | 1997-10-02 | 1999-12-31 | Dassault Electronique | PERFECTED RADIONAVIGATION RECEIVER, ESPECIALLY OF THE GPS TYPE |
JP3522581B2 (en) * | 1999-04-22 | 2004-04-26 | 富士通株式会社 | GPS positioning device, GPS positioning method, and computer-readable recording medium recording GPS positioning program |
US6732050B2 (en) * | 2001-05-23 | 2004-05-04 | Nokia Mobile Phones Ltd | Two-stage interacting multiple models filter for use in a global positioning system |
FR2830320B1 (en) * | 2001-09-28 | 2003-11-28 | Thales Sa | HYBRYDAL INERTIAL NAVIGATION CENTER WITH IMPROVED INTEGRITY |
US6781542B2 (en) * | 2003-01-13 | 2004-08-24 | The Boeing Company | Method and system for estimating ionospheric delay using a single frequency or dual frequency GPS signal |
-
2005
- 2005-01-20 FR FR0500592A patent/FR2881008B1/en not_active Expired - Fee Related
-
2006
- 2006-01-03 DE DE602006002367T patent/DE602006002367D1/en active Active
- 2006-01-03 US US11/814,409 patent/US7504996B2/en active Active
- 2006-01-03 CA CA2589463A patent/CA2589463C/en active Active
- 2006-01-03 AT AT06700317T patent/ATE405852T1/en not_active IP Right Cessation
- 2006-01-03 WO PCT/EP2006/050014 patent/WO2006077174A1/en active IP Right Grant
- 2006-01-03 EP EP06700317.8A patent/EP1839070B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP1839070A1 (en) | 2007-10-03 |
FR2881008A1 (en) | 2006-07-21 |
US20080129586A1 (en) | 2008-06-05 |
DE602006002367D1 (en) | 2008-10-02 |
CA2589463C (en) | 2015-11-10 |
US7504996B2 (en) | 2009-03-17 |
ATE405852T1 (en) | 2008-09-15 |
EP1839070B2 (en) | 2014-04-30 |
EP1839070B1 (en) | 2008-08-20 |
CA2589463A1 (en) | 2006-07-27 |
WO2006077174A1 (en) | 2006-07-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20130930 |